This light helicopter was built and flown in 2001 by the Lada Land company based in Tolyatti, Russia.

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Technical data for Lada Land VM-01 Engine: 1 x 170hp VAZ-416 piston engine , main rotor diameter: 9.00m, tail rotor diameter: 1.56m, max take-off weight: 890kg, payload: 300kg, cruising speed: 140km/h, rate of climb: 240m/min, ceiling: 3000m, range: 330km/h

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